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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 17 18 19 20 21 Next > Last >>
HN93-F3B.320 8.85 30 2.146 40 0.942 0.0059
HN93-F3F.323 8.55 30 2.001 45 1.061 0.0052
HN93-S.800 7.98 25 0 0 0.749 0.0049
HN93-S.885 8.83 25 0 0 0.802 0.0056
HQ2.5/10 9.92 40 2.517 50 1.203 0.0103
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.14 0.51 0.14 -0.29
0.4 0.89 0.4 -0.57
1 1.37 1 -0.92
2 2.03 2 -1.27
4 2.98 4 -1.7
6 3.68 6 -1.98
8 4.22 8 -2.17
10 4.67 10 -2.31
15 5.48 15 -2.49
20 6 20 -2.53
25 6.31 25 -2.49
30 6.46 30 -2.39
35 6.48 35 -2.26
40 6.38 40 -2.09
45 6.19 45 -1.91
50 5.91 50 -1.7
55 5.56 55 -1.49
60 5.14 60 -1.27
65 4.66 65 -1.05
70 4.12 70 -0.83
75 3.54 75 -0.62
80 2.9 80 -0.41
85 2.21 85 -0.23
90 1.48 90 -0.08
95 0.71 95 0.03
100 0 100 0
X Y
1 0
0.95 0.0071
0.9 0.0148
0.85 0.0221
0.8 0.029
0.75 0.0354
0.7 0.0412
0.65 0.0466
0.6 0.0514
0.55 0.0556
0.5 0.0591
0.45 0.0619
0.4 0.0638
0.35 0.0648
0.3 0.0646
0.25 0.0631
0.2 0.06
0.15 0.0548
0.1 0.0467
0.08 0.0422
0.06 0.0368
0.04 0.0298
0.02 0.0203
0.01 0.0137
0.004 0.0089
0.0014 0.0051
0 0
0 0
0.0014 -0.0029
0.004 -0.0057
0.01 -0.0092
0.02 -0.0127
0.04 -0.017
0.06 -0.0198
0.08 -0.0217
0.1 -0.0231
0.15 -0.0249
0.2 -0.0253
0.25 -0.0249
0.3 -0.0239
0.35 -0.0226
0.4 -0.0209
0.45 -0.0191
0.5 -0.017
0.55 -0.0149
0.6 -0.0127
0.65 -0.0105
0.7 -0.0083
0.75 -0.0062
0.8 -0.0041
0.85 -0.0023
0.9 -0.0008
0.95 0.0003
1 0
X Y
100 0
95 0.71
90 1.48
85 2.21
80 2.9
75 3.54
70 4.12
65 4.66
60 5.14
55 5.56
50 5.91
45 6.19
40 6.38
35 6.48
30 6.46
25 6.31
20 6
15 5.48
10 4.67
8 4.22
6 3.68
4 2.98
2 2.03
1 1.37
0.4 0.89
0.14 0.51
0 0
0 0
0.14 -0.29
0.4 -0.57
1 -0.92
2 -1.27
4 -1.7
6 -1.98
8 -2.17
10 -2.31
15 -2.49
20 -2.53
25 -2.49
30 -2.39
35 -2.26
40 -2.09
45 -1.91
50 -1.7
55 -1.49
60 -1.27
65 -1.05
70 -0.83
75 -0.62
80 -0.41
85 -0.23
90 -0.08
95 0.03
100 0
V 1.1